HIGH ENTHALPY AIR FOR HYPERSONIC SHOCK TUNNEL TESTING

• 1. 一种用于钻爆隧道洞内爆破空气冲击波的预防装置及预防方法 [P] . 中国专利： CN104315934A . 2015-01-28
• 2. 一种用于钻爆隧道洞内爆破空气冲击波的预防装置 [P] . 中国专利： CN204495212U . 2015.07.22
• 3. METHOD FOR DETERMINING TURNING ANGLE OF THRUST VECTOR OF HYPERSONIC ONCE-THROUGH AIR JET ENGINE WITH CHAMFER CUT OF NOZZLE AS PER RESULTS OF FLIGHT TESTS ON HYPERSONIC FLYING LABORATORY [P] . 俄罗斯专利： RU2445599C1 . 2012-03-20

  机译： 超音速飞行实验室飞行试验结果确定带有喷嘴倒角的超音速一次通过式喷气发动机推力矢量转角的方法

• 4. Low cost wind tunnel for supersonic and hypersonic aerothermal testing [P] . 美国专利： US7401505B1 . 2008-07-22

  机译： 用于超音速和高音速空气热测试的低成本风洞

• 5. FREE JET HYPERSONIC WIND TUNNEL TESTING APPARATUS [P] . 日本专利： JP2002340733A . 2002-11-27

  机译： 免费的JET超音速风洞测试设备

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• 3. Wind Tunnel Test and Numerical Computation on Ice Accretion on Blade Airfoil for Straight-bladed VAWT [J] . LI Shengmao, LI Yan, FENG Fang, 东北农业大学学报（英文版） . 2010,第004期
• 4. Calspan's Upgraded 96" Hypersonic Shock Tunnel: Its Development and Application in the performanceof Research Testing at Higher Enthalpies [C] . T.Albrechcinski, D.Boyer, K.Chadwick, AIAA 33rd Aerospace Sciences Meeting and Exhibit 9502957 January 9-12, 1995/Reno, NV . -1
• 5. Design, calibration and testing of a force balance for a hypersonic shock tunnel. [D] . Vadassery, Pravin. 2012
• 6. Construct validity test–retest reliability and internal consistency of the Thai version of the disabilities of the arm shoulder and hand questionnaire (DASH-TH) in patients with carpal tunnel syndrome [O] . Montana Buntragulpoontawee, Suphatha Phutrit, Siam Tongprasert, 2018
• 7. Design/Construction and Performance Test of Hypersonic Shock Tunnel Part Ⅰ: Design Method of Hypersonic Shock Tunnel [O] . 2008
• 8. Closely Coupled Experimental and Numerical Approach for Hypersonic and High Enthalpy Flow Investigations Utilising the HEG Shock Tunnel and the DLR TAU Code. [R] . A. Wagner J. M. Schramm K. Hannemann S. Karl V. Hannemann 2010

• 1. Processing the rig test data of an air filling twin-tube shock absorber [J] . 董明明 ,骆振兴 ,赵永飞 . 北京理工大学学报：英文版 . 2015,第2期
• 2. Wind Tunnel Test for Videogrammetric Deformation Measurement of UAV for Mars Airplane Balloon Experiment-1 (MABE-1) [J] . Koji Fujita ,Akira Oyama ,Daisuke Kubo . 流量控制、测量及可视化（英文） . 2019,第2期
• 3. 高焓超音速气流中气体取样分析 [C] . 郑必可 ,陈立红 ,林然 . 第六届全国实验流体力学学术会议 . 2004
• 4. 基于空气焓值法的房间空调器能效测试系统的设计与性能分析 [A] . 王泉 . 2016